GE CF6-80 series
Service difficulty reports · 1,092
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'CF680' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'CF680' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201203311201Pressure Switch · failedNR 2 ENGINE FUEL FILTER CLOG ECAM/ MASTER CAUTION IMMEDIATELY AFTER TAKE OFF. ECAM CAUTION EXTINGUISHED AROUND 80 PERCENT N1 WHEN THROTTLES RETARDED. REMOVED AND INSPECTED NR 2 ENGINE FUEL FILTER. NO DEBRIS FOUND. INSTALLED NEW FILTER IAW MM 73-12-03-02.SDR HALA2012031800112Compressor · stalledNR 2 ENGINE COMPRESSOR STALL AT TOP OF CLIMB. FLT CREW DECLARED EMERGENCY AND DIVERTED BACK, WHERE AN UNEVENTFUL LANDING WAS MADE. OPEN.SDR IPXA2672408Wire · chafedON TAKE OFF, THE RT ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CHECKED AND REPLACED THE RT ENGINE OIL FILTER, IT WAS CLEAN. FOUND CHAFED WIRE FOR FILTER PRESSURE SWITCH. REPAIRED WIRE.SDR FDEA201203020770Line · leakingON ARRIVAL, FOUND LARGE AMOUNT OF FUEL DRAINING FROM DRAIN MAST OF NR 1 ENGINE. OPENED NR 1 ENGINE CORE COWL AND FOUND MAIN FUEL LINE SPRAYING FUEL AT THE FIREWALL CONNECTION. PULLED FIRE HANDLE AND DISCONNECTED FUEL LINE AT THE FIREWALL AND FOUND RETAINER SDR HALA2012022900093Engine · hung startLEFT ENGINE HUNG START, FUEL FLOW AND DUCT PRESSURE WERE NORMAL. HUNG AT 56 PERCENT N2 AND EGT 710 DEGREES WHEN START ABORTED. SECOND START NORMAL. GROUND START 1 & 2, NO DEFECTS NOTED ON NR 1 ENGINE.SDR UIEA2012012400026Gasket · leakingENGINE NR 4 FAIL. NORMAL PARAMETERS DURING TAKEOFF AND INITIAL CLIMB. ROLLED BACK TO IDLE ABOUT 20,000 FT. FAIL DURING DESCENT. AIR TURN BACK. WINDMILLED ABOUT 40 MINUTES. FOUND FUEL LEAK AT FUEL OUT CONNECTION AT FCOC GASKET.SDR WRLA20120120535Line · looseCREW REPORTED THAT APPROX 2 HOURS INTO FLIGHT THEY NOTICED THAT THE NR 2 ENG OIL QUANTITY WAS DROPPING. THE OIL QUANTITY CONTINUED TO DROP AT AN APPROX RATE OF 1 QT PER HOUR. OIL PRESS AND TEMP REMAINED NORMAL. APPROX 1 HOUR PRIOR TO LANDING THE OIL QTY WASSDR WRLA20120113531Door Frame · corrodedFOUND MAIN DECK DOOR FRAME HAS CORROSION AT L18-19R. REPAIRED IAW EI W2012A53B-095 REV 00,01, & 02.SDR WRLA20120113532Skin · corrodedDURING 2C CHECK, FOUND CORROSION ON EXTERNAL UPPER SURFACE OF RT WING UPPER SKIN BETWEEN WING STATION XCW 118- XORS 949. REPAIRED IAW EI W2012A57B-089 REV:00, REV:01 & REV:02.SDR WRLA20120102533Fuel Cell · corrodedFOUND CORROSION ON CENTER WING TANK UPPER SURFACE AT XCW = 96.5 S-15-S-18. REPAIRED IAW EI W2012A57B-051. REV:00, REV:01 & REV:02SDR WRLA20120101530Fuel Cell · corrodedDURING 2C CHECK, MECHANICS FOUND CORROSION ON CENTER WING TANK UPPER SKIN SURFACE AT XCW = 99.0 S-15. REPAIR ACCOMPLISHED AS PER EGAT EI NO: W2012A57B-027 REV:00, REV:01 & REV:01.SDR IPXA11670859Escape Reel · unwanted deployDURING GROUND CHECK, EMERGENCY DESCENT DEVICE CABLE DEPLOYED. REPLACED IAW EMERGENCY DESCENT DEVICE IAW MM 25-61-03-2.SDR WRLA20111120526Switch · inoperativeR1 DOOR SLIDE PRESS TO TEST INOP AND PUSHED BEGIN PANEL. REFITTED SWITCH IN DOOR PANEL AND REPLACED BATTERIES AND PUSH BUTTON FROM L1 DOOR R1 TESTS OK. ISSUED DMI FOR THE L1 DOOR PRESS TO TEST.SDR FDEA201111104854Unknown · unknownON CLIMB OUT THRU 16,000 HAD LOUD RUMBLE AND ACFT SHOOK BRIEFLY. HAPPENED 6 OR 7 MORE TIMES. DID NOT NOTICE ANY ABNORMAL INDICATIONS. RETURNED BACK TO FIELD. INSPECTED AIRCRAFT, NO DEFECTS FOUND.SDR FDEA201111084820Accelerometer · malfunctionedREJECTED TAKE OFF, DUE TO NR1 ENGINE EVM COMPRESSO AMBER BOX ILLUMINATED AT APPROX 5.0 THEN EXTINGUISHED, FOLLOWED BY ILLUMINATION OF THE NR 1 ENGINE EVM TURBINE AMBER BOX AT APPROX 4.4. NO PHYSICAL VIBRATION. PER FIM 77-32 INSPECTED NR 1 ENG FOR DAMAGE. NSDR IXXA110070OWarning Light · illuminatedDURING CRUISE, THE MAIN CARGO DOOR LIGHT ILLUMINATED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. OPENSDR FDEA201110144491Compressor · stalledON CLIMBOUT PASSING FL 260 ENGINE NR 1 COMPRESSOR STALLED, EVM COMP STARTED VIBRATION 4.8 UPD TO 5.0,N1 DROPPED FROM 102.5 TO 96, EGT RISE TO 580. ON ACFT ARRIVAL FIRST INSP FOUND ALL TURBINE BLADES DAMAGED MOCC P/P CONSULTED. REMOVED AND REPLACED NR 1 ENGINSDR FDEA201108093148Indicator · inoperativeR1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATOR INOPERATIVE. R & R 2 BATTERIES IAW MM:25-61-04-4-0. OPS CHECK OK. ACFT OK TO CONTINUE.SDR WRLA20110806498Fire Bottle · brokenAPU FIREX BOTTLE INADVERTENLY FIRED AT A-6 CHECK. DISCHARGE HEAD AT BOTTLE BROKE RELEASING AGENT INTO AFT ASSY COMPARTMENT NOT TO APU DISCHARGE TUBES AC TT 64151:56 TC 12530.SDR WRLA20110726496Mount · brokenREPORT R3 DOOR DISARMED LIGHT ILLUMINATED ON LANDING. UPON INSPECTION FOUND THE AFT GIRT BAR MOUNT BROKEN. SWAPPED NR 4R GIRT-BAR BRACKET WITH DOOR 3R. ALL FASTENERS TORQUED IAW 20-50-00 - SLIDES REFITTED IAW 25-61-22. OPS CHECK OF R3 DOOR ARM INDICATION SSDR WRLA20110717493Bottle · low pressureL-1 DOOR BOTTLE LOW. SERVICED L-1 DOOR ASSIST BOTTLE.SDR FDEA201107132674Skin · dentedRAMP REPORTED DENT 17 IN AFT OF FWD LOWER CARGO DOOR AND APPROX 57 IN UP FROM BOTTOM OF DOOR OPENING. INSP IAW SRM 53-10-12 DIAGRAM 109 WITIN LIMITS OF "B" NO REPAIR REQUIRED. REINSPECT WITHIN 3000 FC. ACFT OK TO CONTINUE. NO RESTRICTION REF: SRM 53-10SDR HALA2011070700312Bleed Valve · malfunctionedETOPS SIGNIFICANT SYS - LT ENG HPSOV NOT OPERATING NORMALLY. NO BLEED ABOVE 10PSI W/60 PERCENT N1. RETURNED TO GATE. FOUND HP BLEED DUCT CLAMP NOT INSTALLED. INSTALLED E-SEAL & CLAMP. PNEU LEAK CHECKED GOOD.SDR IPXA1667347Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL POS 2/3 HAS 1EA HOLE. REF D432191, FABRICATED & REPLACED FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA1667348Floor Panel · damagedREF D431900, FLOOR PANEL 2L HAS 1" HOLE. FABRICATED & REPLACED PANEL IAW EO B767-5320-9693-H.SDR IPXA11667324Floor Panel · brokenINSPECTION TYPE:8C, MCD FLOOR PANEL FOUND BROKEN AND TOGETHER WITH 5 DENT MARKS AT STA 731 TO 833, RBL55 TO RBL77. FLOOR PANEL FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.SDR IPXA1M67005Skin · gougedINSPECTION TYPE:4C, RT WING UPPER SURFACE NEAR L/E JUST ABOVE SLAT TRACK NR3 APPROX XIS247 REPAIR DOUBLER FOUND GOUGED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT REPAIR DOUBLER ON RT EXTERIOR AT XIS 247 IAW EO MD11-5750-42888-A AND STASA EA 011-5750- 01-SDR HALA2011041600157Transmitter · out of adjustETOPS SIGNIFICANT SYS. ON TAXI CHECK SELECTING FLAP 5, NOTICED A SIGNIFICANT DIFFERENCE IN AILERON DROOP FROM LT TO RT. BITE FSEU & PSEU NO FAULTS NOTED. NO EICAS MSGS. VERIFIED INBD AILERON SPLIT. CHECKED INBD AILERON DROOP IAW AMM 27-11-06, CK OK, CK INSDR FDEA201104091414Gearbox · dirtyLOWERED FLAPS TO 20*, 5 SEC LATER RECEIVED ECAM FLAPS SYS 1 & 2 FAULT. RECYCLED, WHICH FIXED PROBLEM. THEN TRIED TO CONFIGURE FLAPS 40*, RECEIVED SAME ECAM FLAPS SYS 1 & 2 FAULT. FLAPS STUCK AT 15*/20*. REPLACED LEFT TEE GEARBOX PER AMM 27-54-14. REPSDR FDEA201104061367Transmitter · inoperativeBLUE RESOVOIR LO LEVEL AT FL 310/ BLUE PUMP OFF REMAINDER OF FLIGHT. PRIOR TO PUMP SHUTDOWN, PRESSURE 450 PSI. ECAM ALERT AT RED DOT ON OVERHEAD. CREW DECLARED AN EMERGENCY BUT TAXIED TO RAMP/GATE UNDER ACFT ENGINE POWER. AT BLOCK-IN THERE WAS NO SIGNS/EVSDR FDEA201104061335Skin · misrepairedREPAIR FOUND ON CTR CARGO DOOR SKIN FWD LOWER CORNER. REPAIR NOT CARRIED OUT IN ACCORDANCE WITH APPROVED DATA. CENTER CARGO DOOR CARRIED OUT REPAIR AS PER SRM 52-30-16 FIGURE 201 REPAIR 3 REVISION 46. E.O. 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJSDR FDEA201104051323Fuel Filter · contaminatedDURING GO-AROUND WITH APPROX 4.5 THOUSAND POUNDS OF FUEL IN EACH OUTER TANK, NR 1 ENG FUEL CLOG LIGHT ILLUMINATED. IT EXTINGUISHED, THEN RE-ILLUMINATED IN LEVEL FLIGHT, THEN EXTINGUISHED. NO ENGINE SECONDARIES. CREW REPORTED NO NOTICED FLUCTUATION OF NR 1SDR FDEA201104041310Skin · crackedLT WING - 24 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 TO STA XORS 713.6. REPAIR CARRIED OUT AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS 683.4 TO STASDR FDEA201104031307Frame · misrepairedFRAME REPAIR AT STA 535 LT, L-18, -L21. EVALUATED AND FOUND NOT REPAIRED IAW APPROVED DATA. CARRIED OUT REPAIR IAW DWG SG10530002, REV 0. EO 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.SDR HALA2011040200146Power Supply · inoperativeEXTERNAL EMERGENCY LIGHT BETWEEN LT OVERWING EXITS INOP. R & R M736 POWER SUPPLY CHARGER ASSY IAW AMM33-51-07, OPS CHECK OK.SDR UIEA2011040100172Frame · damagedDURING "C-CHECK", PREVIOUSLY TIME LIMITED REPAIRED LOWER LOBE FRAME AND FAIL SAFE CHORD WERE FOUND TO HAVE ADDITIONAL DAMAGE. THE REMOVED SECTIONS OF FRAME WEB 65B04315-22 AND FAIL SAFE CHORD 65B04315-1, WERE REPLACED WITH IDENTICAL SECTIONS. THE SPLICED JOSDR FDEA201104011295Skin · misrepairedREPAIR DOUBLER AT LT WING INBD SIDE OF NR 4 SLAT TRACK SLAT INNER SURFACE FOUND NOT CARRIED OUT IAW APPROVED DATA. REMOVED AND NEW REPAIR INSTALLED IAW SRM 57-40-01, FIG 201, REPAIR 3, REV 46. EO 1-5100-7-5001 A5 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMMSDR UIEA2011032800160Eec · malfunctionedAFTER ENGINE START, NR 1 ENGINE WENT TO IMMED T/O THRUST UNCOMMAND. ENGINE SHUTDOWN PERFORMED. FAULT CONFIRMED ON GROUND RUN, 101 PERCENT IN EEC NORMAL MODE. EEC ALT MODE SELECTED AND ENG RUN C/O SATIS. NR 1 ENG ECU REPLACED IAW AMM.SDR UIEA2011032400162Seat Track · crackedDURING D-CHECK INSP, CRACKS WERE FOUND ON SEAT TRACK AT BS 995. THE DAMAGED SEAT TRACK WAS REPAIRED IAW SRM 53-00-52-2R-13, FIG 201.SDR WRLA20110317475Fan · failedOBSERVED ACRID ODOR AND MIST OF SMOKE IN ZONE-A AT APPROXIMATELY FIVE HOURS IN FLIGHT. FOUND C/B'S POPPED FOR NR 1 RECIRC FAN. OPS CHECK FOUND C/BS POPPING. TRANSFERRED TO DMI M21MR1711-132 CAT C DUE DATE 27 MAR 2011. PER MEL 21-22-03-01 C/B'S FOR FAN PULLSDR FDEA201103161013Engine · damagedDURING GEAR RETRACTION AND AFTER GEAR RETRACTED, WE HEARD A GRINDING NOISE AND SMELLED A STRONG ODOR THAT IS SIMILIAR TO SOMETHING BURNING (NOT ELECTRICAL). DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE FOR AN UNEVENTFUL LANDING. TURNED OUT WE HIT A SKUNK OSDR UIEA2011031300150Seat Track · crackedDURING LOADING, THE BS 570, LBL 25 LOWER LOBE SEAT TRACK WAS FOUND CRACKED ON 13MAR2011. THE DAMAGE MEASURES 7 INCHES IN LENGTH. NO CARGO MAY BE CARRIED IN THE LOWER LOBE P-11 AND P-12 POSITIONS UNITL PART 3 IS ACCOMPLISHED. (PART 1 OF THIS EO ACCOMPLISHES ASDR FDEA201103040844Angle · corrodedUPON REMOVAL OF LAV SERVICE BOX AND SKIN STIFFENERS, FOUND EXCESSIVE CORROSION EXTENDING UNDER FR 12A LT AT STR 37L. REMOVED LEVEL ONE CORROSION IAW SRM 51-74-10. MATERIAL LOSS WAS 100 PERCENT OF ANGLE AT FR 12A AND STR 37L, FOUND TO BE OUT OF LIMITS IAW SDR UIEA2011030200137Lens · damagedDURING WALK-AROUND INSP AT PVG, MX FOUND THE LT OTBD LANDING LIGHT - LENS COVER ASSY DAMAGED. (DISPOSITION WAS MADE TO ACCOMPLISH TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, SCHEDULE REPEAT INSP EVERY 1 FC AND PERMANENT REPAIR BY REPLACING TSDR FDEA201103020827Rib · crackedRT WING INBD FLAP, T/E OF RIB 25A, 02 EA HOLES FOUND CRACKED INDICATION DURING HIGH FREQUENCY EDDY CURRENT INSP. CRACKED RIB 25A AT RT WING INBD FLAP R & R IAW SRM 51-40-21, REV 19. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.SDR FDEA201102220665Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FR 78 SEAT TRACK 2R CORRODED IN THE SCALLOP APPROX 1 SQ INCH. REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10, CHECKED LIMITS, FOUND TO BE OUT OF LIMIT IAW SRM 53-10-16, PAGE 201. R & R SEAT TRACK 2R FROM FR 76 TO FR80 IAW SRM 53-10 16SDR FDEA201102210645Web · crackedFWD CARGO COMPARTMENT UNDER FLOOR VERTIVAL WEB IS CRACKED BETWEEN FRAME 36 & FRAME 37; LBL 56. UPPER AND LOWER WEBS WERE REMOVED IAW SRM 51-40-21, PARA 6. NEW WEBS LOCATED AND DRILLED IAW SRM 51-40-44, PAGE 1. BOTH WEBS INSTALLED IAW SRM 51-40-21, PARA 7.SDR FDEA201102210646Web · crackedFWD CARGO COMPARTMENT UNDER FLOOR VERTICAL WEB IS CRACKED BETWEEN FRAME 37 & FRAME 38; LBL 56. REMOVED AND REINSTALLED PALLET LATCH AT FRAME 37, RBL 33 IAW AMM 25-52-34- 04, PARA 2B1 & 2E2. REMOVED AND REINSTALLED PDU TRAY AT FRAME 37 TO 38 RT IAW SRM 51-4SDR FDEA201102200635Light · illuminatedEMERGENCY POWER ON LIGHT CAME ON DURING FLIGHT - FOLLOWED QRH IT WENT OUT. ADJUSTMENT TEST POWER SYS EMERGENCY IAW AMM 24-24-00-5. OPS CHECKED GOOD, ACFT OK FOR SERVICE AT THIS TIME. FINAL CLOSED.SDR HALA2011022000108Warning Message · false activationETOPS SIGNIFICANT SYS - EICAS MESSAGE AILERON LOCKOUT ILLUMINATED AT HIGH SPEED (270 KTS ACCELERATING) FOR 2 MIN THEN EXITINGUISHED. OTBD AILERONS INDICATED NORMAL-LOCKED OUT. TROUBLESHOT IAW FIM 27-11-00-1, FIG 104, FOUND TO BE OK FOR SERVICE.
Back to GE CF6-80 series